EP3919675A1 - Segment de garniture de raffinage pour un raffineur - Google Patents

Segment de garniture de raffinage pour un raffineur Download PDF

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Publication number
EP3919675A1
EP3919675A1 EP20178487.3A EP20178487A EP3919675A1 EP 3919675 A1 EP3919675 A1 EP 3919675A1 EP 20178487 A EP20178487 A EP 20178487A EP 3919675 A1 EP3919675 A1 EP 3919675A1
Authority
EP
European Patent Office
Prior art keywords
blade segment
blade
edge
longitudinal axis
refiner
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP20178487.3A
Other languages
German (de)
English (en)
Inventor
Marko Loijas
Tomi Iisakkila
Håkan SJÖSTRÖM
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Valmet Technologies Oy
Original Assignee
Valmet Technologies Oy
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Valmet Technologies Oy filed Critical Valmet Technologies Oy
Priority to EP20178487.3A priority Critical patent/EP3919675A1/fr
Priority to CN202180040543.4A priority patent/CN115698423A/zh
Priority to BR112022023725A priority patent/BR112022023725A2/pt
Priority to PCT/EP2021/064841 priority patent/WO2021245161A1/fr
Priority to KR1020227041230A priority patent/KR20230020403A/ko
Priority to US18/007,679 priority patent/US20230228033A1/en
Priority to CA3179136A priority patent/CA3179136A1/fr
Priority to JP2022574530A priority patent/JP2023527922A/ja
Publication of EP3919675A1 publication Critical patent/EP3919675A1/fr
Pending legal-status Critical Current

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Classifications

    • D—TEXTILES; PAPER
    • D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21D—TREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00—Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20—Methods of refining
    • D21D1/22—Jordans
    • D21D1/24—Jordan rolls
    • D—TEXTILES; PAPER
    • D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21D—TREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00—Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20—Methods of refining
    • D21D1/22—Jordans
    • D21D1/26—Jordan bed plates
    • D—TEXTILES; PAPER
    • D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21D—TREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00—Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20—Methods of refining
    • D21D1/30—Disc mills
    • D21D1/306—Discs

Definitions

  • the invention relates to refiners for refining fibrous material and especially to a blade segment for a refiner for refining fibrous material.
  • Refiners used for refining fibrous material comprise typically two refining elements opposite to each other and turning relative to each other, i.e. one or both of them is/are rotating.
  • the refining elements comprise refining surfaces provided with blade bars and blade grooves therebetween, the blade bars being intended to defiber and refine the material to be refined and the blade grooves being intended to convey the material to be refined forward along the refining surfaces.
  • the refining surface of the refining element is typically formed of several blade segments fastened to a body of the respective refining element, each blade segment comprising a respective refining surface formed by blade bars and blade grooves therebetween.
  • the complete refining surface of the refining element is thus formed of the refining surfaces of several blade segments fastened next to each other in the refining element.
  • EP-publication 3401439 B1 discloses a blade segment applicable to be used in refiners for refining fibrous material.
  • An object of the present invention is to provide a novel blade segment for a refiner for refining fibrous material, as well as a novel refiner for refining fibrous material.
  • the invention is characterized by the features of the independent claim.
  • the invention is based on the idea of configuring at least one side edge of the blade segment to provide such a shape that deviates from a direction of a longitudinal axis of the blade segment.
  • the shape of at least one side edge of the blade segment When the shape of at least one side edge of the blade segment is arranged to have a shape that deviates from the direction of the longitudinal axis of the blade segment, and when the configuration of the opposite side edge is selected in co-operation with the configuration of the first mentioned side edge, it provides longitudinal slit-like openings providing flow paths between the neighbouring blade segments for supplying the fibrous material to be refined into the refining chamber between the stator and the rotor and for discharging the fibrous material already refined out of the refining chamber.
  • This slit-like opening has therefore a centre line the direction of which deviates from the direction of the longitudinal axis of the blade segment at least at most part of the extension of the opening.
  • Figure 1 is a schematic general side view of a general construction of a refiner 1 in cross-section, which refiner may be used for refining a fibrous material, such as a wood material containing lignocellulose or another fibre material suitable to be used for manufacturing paper or paperboard, for example.
  • the refiner 1 shown in Figure 1 is of conical type but disc-refiners, conical-disc-refiners and cylindrical refiners could be used as well as an example here.
  • a refiner comprises at least two substantially oppositely positioned refining elements at least one of which is rotating, and a refining chamber formed between each two substantially oppositely positioned refining elements. In the following a refiner with only one rotatable refining element is described.
  • the refiner 1 of Figure 1 comprises a frame 2 and a stationary, fixed refining element 3, i.e. a stator 3, supported on the frame 2.
  • the stator 3 comprises two or more stator blade segments 4, each of them comprising blade bars and blade grooves therebetween.
  • the blade bars and the blade grooves in each stator blade segment 4 form a refining surface 5 of the respective blade segment 4, the refining surface 5 of each stator blade segment 4 thereby providing a part of a refining surface of the stator 3.
  • a complete refining surface of the stator 3 is formed of the refining surfaces 5 of a necessary number of the blade segments 4 fastened next to each other in the stator 3 so that the complete refining surface 5 extending over the whole circumference of the stator 3 is provided.
  • both the refining surface of each single stator blade segment 4 as well as the complete refining surface of the stator 3 are herein denoted with the same reference sign 5.
  • the refiner 1 further comprises a rotatable refining element 6, i.e. a rotor 6, of the refiner 1.
  • the rotor 6 comprises a hub 7.
  • the rotor 6 further comprises two or more rotor blade segments 8 supported to the hub 7, each rotor blade segment 8 comprising blade bars and blade grooves therebetween.
  • the blade bars and the blade grooves in each rotor blade segment 8 form a refining surface 9 of the respective blade segment 8, the refining surface 9 of each rotor blade segment 8 thereby providing a part of a refining surface of the rotor 6.
  • a complete refining surface of the rotor 6 is formed of the refining surfaces 9 of a necessary number of the blade segments 8 fastened next to each other in the rotor 6 so that the complete refining surface 9 extending over the whole circumference of the rotor 6 is provided.
  • both the refining surface of each single rotor blade segment 8 as well as the complete refining surface of the rotor 6 are herein denoted with the same reference sign 9.
  • the hub 7 of the rotor 6 is connected to a driving motor 10 by a shaft 11 so that the rotor 6 can be rotated relative to the stator 3 in a direction of arrow RD, for instance, the arrow RD thus indicating an intended rotation direction RD of the rotor 6.
  • the refiner 1 may also comprise a loading device which, for the sake of clarity, is not shown in Figure 1 .
  • the loading device can be used for moving back and forth the rotor 6 attached to the shaft 11, as schematically shown by arrow A, in order to adjust a size of a refining gap 12, i.e. a refining chamber 12, between the stator 3 and the rotor 6, wherein the fibrous material is actually refined.
  • the fibrous material to be refined is fed into the refiner 1 via a feed channel 13 in a manner shown by arrow F.
  • most of the fibrous material fed into the refiner 1 passes, in a manner schematically shown by arrows P, through openings 14, i.e. flow paths, in the refining surface 9 of the rotor 6 into the refining chamber 12, wherein the fibrous material is to be refined.
  • most of the already refined fibrous material is, in turn, discharged through openings 15, i.e. flow paths, in the refining surface 9 of the stator 3 into an intermediate space 16 between the frame 2 of the refiner 1 and the stator 3, wherefrom the refined material is removed via a discharge channel 17 from the refiner 1, as schematically shown by arrow D.
  • some of the fibrous material to be fed into the refiner 1 may transfer into the refining chamber 12 from the right end of the refining chamber 12, i.e. from a first end 18 or an inner end 18 of the refiner 1 having a smaller diameter, as seen in Figure 1 .
  • some of the already refined material may also exit the refining chamber 12 from the left end of the refining chamber 12, i.e. from a second end 19 or an outer end 19 of the refiner 1 having a larger diameter, as seen in Figure 1 , wherefrom a connection is provided to the intermediate space 16.
  • first end 18 of the refiner 1 In the embodiment of Figure 1 of the refiner 1, only one feed channel 13 is provided, and it is arranged at the first end 18 of the refiner 1 having the smaller diameter.
  • the actual implementation of the refiner could also comprise a second feed channel arranged at the second end 19 of the refiner 1 having the larger diameter, whereby the discharge channel 17 of the refiner 1 could be arranged for example somewhere between the first 18 and second 19 ends of the refiner 1.
  • the reference sign 18 and the term first end 18 or the term inner end 18 may indicate both the first end 18 or the inner end 18 of the refiner 1 having the smaller diameter and the first end 18 or the inner end 18 of the refining element 3, 6 or of the refining chamber 12 having the smaller diameter.
  • the reference sign 19 and the term second end 19 or the term outer end 19 may indicate both the second end 19 or the outer end 19 of the refiner 1 having the larger diameter and the second end 19 or the outer end 19 of the refining element 3, 6 or of the refining chamber 12 having the larger diameter.
  • the blade segment of the solution described herein may be applied in other kind of conical refiners too.
  • the blade segment of the solution described herein is applicable also in cylindrical refiners and disc refiners as well as in refiners comprising both a conical portion and a disc portion.
  • Figure 2 is a schematic oblique side view of a stator 3 and a rotor 6 of a conical refiner, the stator 3 being shown in cross-section.
  • the stator 3 In the circumferential direction of the stator 3 there are a number of adjacent inner blade segments 4a on the side of the inner end 18 of the stator 3 and a respective number of adjacent outer blade segments 4b on the side of the outer end 19 of the stator 3, which inner 4a and outer 4b segments together provide a blade segment 4.
  • Each inner blade segment 4a is interconnected with the respective outer blade segment 4b at the corresponding circumferential position of the stator 3, providing a blade segment 4 that provides a substantially continuous refining surface 5 between the inner end 18 and the outer end 19 of the stator 3 at the respective inner 4a and outer 4b stator blade segments of this blade segment 4.
  • Side edges of the stator blade segments 4a, 4b are implemented such that slit-like openings 15 making flow paths are provided between the interconnected stator blade segments 4 in the circumferential direction of the stator 3.
  • each inner blade segment 8a is interconnected with the respective outer blade segment 8b at the corresponding circumferential position of the rotor 6, providing a blade segment 8 that provides a substantially continuous refining surface 9 between the inner end 18 and the outer end 19 of the rotor 6 at the respective inner 8a and outer 8b stator blade segments of this blade segment 8.
  • FIG. 3 is a schematic planar upper view of a set of adjacent interconnected stator blade segments 4a, 4b or rotor blade segments 8a, 8b applicable to be used for forming a part of the refining surface 5, 9 of a stator 3 or a rotor 6 substantially similar to that of Figure 2 .
  • Figure 4a shows schematically a planar upper view of a blade segment 4a, 8a applicable to be used on the side of the inner end 18 of the stator 3 or the rotor 6
  • Figure 4b shows schematically a planar upper view of a blade segment 4b, 8b applicable to be used on the side of the outer end 19 of the stator 3 or the rotor 6.
  • Figures 5 and 6 disclose schematically a planar upper view of another blade segment 4, 8 applicable to be used in a stator 3 and/or a rotor 6 of a conical refiner, the refining surface 5, 9 of the blade segment 4, 8 being omitted in Figures 5 and 6 for the sake of clarity.
  • the blade segment 4, 8 of Figures 5 and 6 is intended to extend as a single uniform piece from the inner end 18 of the stator 3/rotor 6 up to the outer end 19 of the stator 3/rotor 6.
  • the following description is thus applicable to each blade segment 4, 4a, 4b, 8, 8a, 8b mentioned above, including the blade segments 4, 8 being formed by interconnecting the inner 4a, 8a and respective outer 4b, 8b blade segments.
  • the blade segment 4, 4a, 4b, 8, 8a, 8b comprises an inner end edge 20 or a first end edge 20 to be directed towards the inner end 18 of the refining element 3, 6 having the smaller diameter.
  • the blade segment further comprises an outer end edge 21 or a second end edge 21 to be directed towards the outer end 19 of the refining element 3, 6 having the larger diameter.
  • the inner end edge of the blade segment provides an axially inner end of the blade segment and the outer end edge of the blade segment provides an axially outer end of the blade segment, the direction from the axially inner end towards the axially outer end thus providing the longitudinal axis of the blade segment.
  • the outer end edge 21 is thus substantially opposite to the inner end edge 20 in the direction of the longitudinal axis of the blade segment.
  • the longitudinal axis LA of the blade segment is shown schematically by arrows both at a centre line of the blade segments as well as at an edge line of the blade segments, which lines have a common intersecting point.
  • Below the longitudinal axis LA at the edge line of the blade segment is also called edge axis and is denoted with the reference sign LA' and shown with broken lines in Figure 6 .
  • Figures 4a, 4b and 5 the longitudinal axes of the blade segments are shown schematically at centre lines of the blade segments.
  • a line denoting the longitudinal axis LA of the blade segment actually runs along the conical surface of the blade segment and therefore runs at an angle relative to the shaft 11 of the conical refiner 1 but may be projected at the shaft 11 so as to run parallel to the shaft 11 of the refiner 1.
  • a line denoting the longitudinal axis LA of the blade segment running along the cylindrical surface of the blade segment runs substantially parallel to the shaft of the refiner.
  • a line denoting the longitudinal axis LA of the blade segment runs along a substantially planar surface of the blade segment in a radial direction of the blade segment, i.e. in disc-like blade segments the longitudinal axis of the blade segment unites with the radial direction of the blade segment.
  • the blade segment further comprises a first side edge 22 or a leading side edge 22 extending from the inner end edge 20 of the blade segment up to the outer end edge 21 of the blade segment and providing the side edge of the blade segment which first meets the edge of a counter blade segment during operation of the refiner, to be directed substantially towards the intended rotation direction RD of the rotor 6. So, in the rotor 6 it provides the side edge of the blade segment to be directed towards the intended rotation direction RD of the rotor 6 and in the stator 3 it provides the side edge of the blade segment to be directed to opposite direction relative to the intended rotation direction RD of the rotor 6.
  • the blade segment further comprises a second side edge 23 or a trailing side edge 23 substantially opposite to the first side edge 22 in a direction substantially perpendicular to the longitudinal axis LA of the blade segment and extending from the inner end edge 20 of the blade segment up to the outer end edge 21 of the blade segment and providing the side edge of the blade segment which last meets the edge of a counter blade segment during operation of the refiner. So, in the rotor 6 it provides the side edge of the blade segment to be directed to the opposite direction relative to the intended rotation direction RD of the rotor 6 and in the stator 3 it provides the side edge to be directed towards the intended rotation direction RD of the rotor 6.
  • the inner 20 and the outer 21 end edges together with the first 22 and second 23 side edges define a periphery of the blade segment 8.
  • the blade segment comprises a body 24 having a front surface 25 to be directed towards the refining chamber 12 of the refiner 1.
  • the front surface 25 of the blade segment body 24 is provided with blade bars 26 and blade grooves 27 which together provide the refining surface 5, 9 of the blade segment.
  • the blade bars 26 are intended to defibre and refine the material to be refined and the blade grooves 27 are intended to convey the material to be refined forward along the refining surface 5, 9.
  • Fastening holes 28 are intended to receive fastening means, like bolts, for fastening the blade segment to the supporting structures pf the stator and the hub of the rotor directly or via fastening elements, like rings, 29, 30 or the like.
  • an extension or shoulder 50, 51, 52, 53 at least on one side edge 22, 23 of the segment.
  • the extension or shoulder is intended to come into contact with a neighbouring blade segment when assembled to provide a part of a refining surface of a refining element of a refiner.
  • Figure 4a and Figure 5 show the shoulders 50, 51 at the inner end of the blade segments 4, 4a, 8, 8a and Figure 4b and Figure 5 show the shoulders 52, 53 at the outer end of the blade segments 4, 4b, 8, 8b.
  • the shoulders 50, 51, 52, 53 may lie on corners of one segment as in Figure 5 , or on corners of separate successive segments, i.e.
  • edge axes LA' along the shoulder lines 50, 51, 52, 53, more specifically via the seam lines between the two neighbouring segments, and running parallel to the axial direction of the refiner (or the radial direction in case of a disc refiner) just like the longitudinal axis LA of the segment.
  • the slit-like opening 14, 15 is formed on the first side edge 22 between the inner shoulder 50 and the outer shoulder 52, and on the second side edge 23 between the inner shoulder 51 and the outer shoulder 53.
  • the slit-like longitudinal opening 14, 15 may run continuously from the innermost shoulder up to the outermost shoulder without interruptions other than those caused by ex-segment structures, like fastening rings.
  • the slit-like longitudinal opening 14, 15 may be discontinuous between the innermost and outermost shoulders when the elbows are designed to have a contact with the neighbouring segment, as disclosed in more detail later.
  • the first side edge 22 comprises, in a direction from the inner end edge 20 towards the outer end edge 21, at least a substantially straight first long edge portion 31.
  • the direction of the first long edge portion 31 is arranged to deviate from the direction of the longitudinal axis LA of the blade segment, i.e. with respect to the direction of the longitudinal axis LA of the blade segment, such that the first long edge portion 31 is directed towards the centre part or the centre line of the blade segment, the centre line of the blade segment being denoted in Figures 4a, 4b and 5 by the longitudinal axis LA of the blade segment.
  • the first long edge portion 31 is followed by a first bend 32a, which is turned away from the direction of the first long edge portion 31, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the first long edge portion 31, that is away from the centre part or the centre line of the blade segment.
  • the first bend 32a is followed by a substantially straight or slightly curved short edge portion 32b.
  • the direction of the short edge portion 32b is arranged to deviate from the direction of the longitudinal axis LA to a different direction than the first long edge portion 31, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the first long edge portion 31, that is away from the centre part or the centre line of the blade segment.
  • the short edge portion 32b is followed by a second bend 32c which is turned away from the direction of the first short edge portion 32b, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the short edge portion 32b, that is towards the centre part or the centre line of the blade segment.
  • the first bend 32a, the short edge portion 32b and the second bend 32c provide an elbow 32 in the first side edge 22 of the blade segment.
  • the second bend 32c or the elbow 32 is, in turn, followed by a substantially straight second long edge portion 33 the direction of which is arranged to deviate from the direction of the longitudinal axis LA of the blade segment to the same direction as the first long edge portion 31, i.e. towards the centre part or the centre line of the blade segment.
  • the second long edge portion 33 is thus arranged to deviate with respect to the direction of the longitudinal axis LA to the same direction as the first long edge portion 31.
  • the second side edge 23 of the blade segments 4, 4a, 4b, 8, 8a, 8b comprises, in a direction from the inner end edge 20 towards the outer end edge 21, at least a substantially straight first long edge portion 41.
  • the direction of the first long edge portion 41 is arranged to deviate from the direction of the longitudinal axis LA of the blade segment, i.e. with respect to the direction of the longitudinal axis LA of the blade segment, such that the first long edge portion 41 is directed away from the centre part or the centre line of the blade segment.
  • the first long edge portion 41 is followed by a first bend 42a, which is turned away from the direction of the first long edge portion 41, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the first long edge portion 41, that is towards the centre part or the centre line of the blade segment.
  • the first bend 42a is followed by a substantially straight or slightly curved short edge portion 42b.
  • the direction of the short edge portion 42b is arranged to deviate from the direction of the longitudinal axis LA to a different direction than the first long edge portion 41, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the first long edge portion 41, that is towards the centre line of the blade segment.
  • the short edge portion 42b is followed by a second bend 42c which is turned away from the direction of the first short edge portion 42b, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the short edge portion 42b, that is away from the centre line of the blade segment.
  • the first bend 42a, the short edge portion 42b and the second bend 42c provide an elbow 42 in the second side edge 23 of the blade segment.
  • the second bend 42c or the elbow 42 is, in turn, followed by a substantially straight second long edge portion 43 the direction of which is arranged to deviate from the direction of the longitudinal axis LA of the blade segment to the same direction as the first long edge portion 41, i.e. away from the centre part or the centre line of the blade segment.
  • the second long edge portion 43 is thus arranged to deviate with respect to the direction of the longitudinal axis LA to the same direction as the first long edge portion 41.
  • the first side edge 22 of the blade segment 4, 8 of Figure 5 further comprises another bevel 34 following the second long edge portion 33.
  • the second long edge portion 33 is followed by a third bend 34a, which is turned away from the direction of the second long edge portion 33, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second long edge portion 33, that is away from the centre part or the centre line of the blade segment.
  • the third bend 34a is followed by a second substantially straight or slightly curved short edge portion 34b.
  • the direction of the second short edge portion 34b is arranged to deviate from the direction of the longitudinal axis LA to a different direction than the second long edge portion 33, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second long edge portion, that is away from the centre part or the centre line of the blade segment.
  • the second short edge portion 34b is followed by a fourth bend 34c which is turned away from the direction of the second short edge portion 34b, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second short edge portion 34b, that is towards the centre part or the centre line of the blade segment.
  • the third bend 34a, the second short edge portion 34b and the fourth bend 34c provide a second elbow 34 in the first side edge 22 of the blade segment.
  • the fourth bend 34c or the second elbow 34 is, in turn, followed by a substantially straight third long edge portion 35 the direction of which is arranged to deviate from the direction of the longitudinal axis LA of the blade segment to the same direction as the first 31 and the second 33 long edge portions, i.e. towards the centre part or the centre line of the blade segment.
  • the third long edge portion 35 is thus arranged to deviate with respect to the direction of the longitudinal axis LA to the same direction as the first 31 and the second 33 long edge portions.
  • the second side edge 23 of the blade segment 4, 8 of Figure 5 comprises another bevel 44 following the second long edge portion 43.
  • the second long edge portion 43 is followed by a third bend 44a, which is turned away from the direction of the second long edge portion 43, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second long edge portion, that is towards the centre part or the centre line of the blade segment.
  • the third bend 44a is followed by a second substantially straight or slightly curved short edge portion 44b.
  • the direction of the second short edge portion 44b is arranged to deviate from the direction of the longitudinal axis LA to a different direction than the second long edge portion 43, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second long edge portion, that is towards the centre part or the centre line of the blade segment.
  • the second short edge portion 44b is followed by a fourth bend 44c which is turned away from the direction of the second short edge portion 44b, i.e. to an opposite direction with respect to the direction of the longitudinal axis LA than the second short edge portion 44b, that is away from the centre part or the centre line of the blade segment.
  • the third bend 44a, the second short edge portion 44b and the fourth bend 44c provide a second elbow 44 in the second side edge 23 of the blade segment.
  • the fourth bend 44c or the second elbow 44 is, in turn, followed by a substantially straight third long edge portion 45 the direction of which is arranged to deviate from the direction of the longitudinal axis LA of the blade segment to the same direction as the first 41 and the second 43 long edge portions, i.e. away from the centre part or the centre line of the blade segment.
  • the third long edge portion 45 is thus arranged to deviate with respect to the direction of the longitudinal axis LA to the same direction as the first 41 and the second 43 long edge portions.
  • both side edges 22, 23 of the blade segment comprise at least two edge portions 31, 33, 35, 41, 43, 45 arranged to deviate from the direction of the longitudinal axis LA of the blade segment 4, 4a, 4b, 8, 8a, 8b and being connected by an elbow 32, 34, 42, 44 between each two edge portions 31, 33, 35, 41, 43, 45.
  • the configurations of the side edges 22, 23 are also arranged to deviate from a mirror image with respect to the longitudinal axis LA of the blade segment.
  • At least one side edge 22, 23 of the blade segment 4, 4a, 4b, 8, 8a, 8b comprises at least two edge portions 31, 33, 35, 41, 43, 45 the directions of which are arranged to deviate from the direction of the longitudinal axis LA of the blade segment 4, 4a, 4b, 8, 8a, 8b, and the at least two edge portions are connected by an elbow 32, 34, 42, 44 between each two edge portions 31, 33, 35, 41, 43, 45.
  • the directions of the edge portions at the specific side edge 22, 23 are arranged to deviate to the same direction from the direction of the longitudinal axis LA and the elbow 32, 34, 42, 44 is turned away from the edge portions 31, 33, 35, 41, 43, 45 such that it deviates with respect to the direction of the longitudinal axis LA of the blade segment to the different direction than the edge portions 31, 33, 35, 41, 43, 45.
  • the reach of the elbows 32, 34 may be so arranged that it does not substantially exceed the edge axis LA', whereby a continuous slit-like opening 14, 15 between the neighbouring segments 4, 8 may be provided.
  • the reach of the elbows 42, 44 may be so arranged that the elbow extends up to the edge axis LA', like the elbow 44, or exceeds the edge axis LA', like the elbow 42. If the opposite side edges 22, 23 are not parallel the elbow may exceed the edge axis LA' even to such an extent that it enables contact with a neighbouring segment, whereby a discontinuous slit-like opening 14, 15 between the neighbouring segments 4, 8 may be provided.
  • the disclosed configuration of the side edge of the blade segment provides a shape of gentle zigzag that deviates from the direction of the longitudinal axis of the blade segment.
  • the configuration of the opposite side edge When the configuration of the opposite side edge is selected in co-operation with the configuration of the first mentioned side edge, it provides longitudinal slit-like openings, i.e. flow paths, between the neighbouring blade segments for supplying the fibrous material to be refined into the refining chamber between the stator and the rotor and for discharging the fibrous material already refined out of the refining chamber.
  • This slit-like opening has therefore a centre line the direction of which deviates from the direction of the axis of the blade segment at least at most part of the extension of the opening.
  • the slit-like opening has a width between 10 mm and 25 mm.
  • the edge portions at the same side edge 22, 23 of the blade segment and arranged to deviate to the same direction from the direction of the longitudinal axis LA of the blade segment are substantially parallel.
  • the effect of this is that an opening of substantially constant width is easy to implement between neighbouring blade segments.
  • each side edge of the blade segment comprises at least one elbow.
  • both side edges of the blade segment has a kind of shape of gentle zigzag, preventing thereby a significant portion of the side edge from following the longitudinal axis of the blade segment and thereby preventing a formation of opening portions possibly causing a tendency of vibration of the refiner during the operation thereof.
  • the elbows at the opposite side edges lie on the same normal level with respect to the longitudinal axis LA of the blade segment, the normal of the longitudinal axis LA of the blade segment being schematically shown in Figure 5 with a broken line denoted with the reference sign N.
  • This has the effect of providing an opening with a substantially constant width along the longitudinal extension of the opening.
  • a number of elbows at each side edge 22, 23 is from one to ten, preferably from two to six, or from two to seven, or from two to eight.
  • the deviation of the direction of extension of the opening from the longitudinal axis of the blade segment may be ensured. Too dense zigzag shape of the side edge of the blade segment may result in a perpetual back-and-forth type flow path for the pulp which eventually does not differ so much from the vibrationally possibly undesired design.
  • an angle of the deviation of the elbow from the longitudinal axis LA of the blade segment is about 10 - 90 degrees, preferably from 10 to 60 degrees, and more preferably from 10 to 50 degrees.
  • a direction of an extension of the elbow is substantially parallel to a direction of an extension of a blade bar.
  • the elbow is arranged to form an angle which is substantially parallel to the blade bar angle applied in the blade segment.
  • configurations of the side edges 22, 23 are arranged to deviate from a mirror image with respect to a longitudinal axis of the blade segment, or in other words, the side edges of the blade segment are not mirror images of each other with respect to the longitudinal axis LA of the blade segment.

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EP20178487.3A 2020-06-05 2020-06-05 Segment de garniture de raffinage pour un raffineur Pending EP3919675A1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
EP20178487.3A EP3919675A1 (fr) 2020-06-05 2020-06-05 Segment de garniture de raffinage pour un raffineur
CN202180040543.4A CN115698423A (zh) 2020-06-05 2021-06-02 用于精磨机的刀片节段
BR112022023725A BR112022023725A2 (pt) 2020-06-05 2021-06-02 Segmento de lâmina para um refinador, e, refinador para refinar material fibroso
PCT/EP2021/064841 WO2021245161A1 (fr) 2020-06-05 2021-06-02 Segment de lame pour raffineur
KR1020227041230A KR20230020403A (ko) 2020-06-05 2021-06-02 리파이너용 블레이드 세그먼트
US18/007,679 US20230228033A1 (en) 2020-06-05 2021-06-02 Blade Segment for Refiner
CA3179136A CA3179136A1 (fr) 2020-06-05 2021-06-02 Segment de lame pour raffineur
JP2022574530A JP2023527922A (ja) 2020-06-05 2021-06-02 リファイナのためのブレードセグメント

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20178487.3A EP3919675A1 (fr) 2020-06-05 2020-06-05 Segment de garniture de raffinage pour un raffineur

Publications (1)

Publication Number Publication Date
EP3919675A1 true EP3919675A1 (fr) 2021-12-08

Family

ID=71016408

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20178487.3A Pending EP3919675A1 (fr) 2020-06-05 2020-06-05 Segment de garniture de raffinage pour un raffineur

Country Status (8)

Country Link
US (1) US20230228033A1 (fr)
EP (1) EP3919675A1 (fr)
JP (1) JP2023527922A (fr)
KR (1) KR20230020403A (fr)
CN (1) CN115698423A (fr)
BR (1) BR112022023725A2 (fr)
CA (1) CA3179136A1 (fr)
WO (1) WO2021245161A1 (fr)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3401439B1 (fr) 2017-05-11 2019-10-09 Valmet Technologies Oy Segment de garniture de raffinage pour un raffineur

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3401439B1 (fr) 2017-05-11 2019-10-09 Valmet Technologies Oy Segment de garniture de raffinage pour un raffineur

Also Published As

Publication number Publication date
JP2023527922A (ja) 2023-06-30
CA3179136A1 (fr) 2021-12-09
BR112022023725A2 (pt) 2022-12-20
CN115698423A (zh) 2023-02-03
KR20230020403A (ko) 2023-02-10
WO2021245161A1 (fr) 2021-12-09
US20230228033A1 (en) 2023-07-20

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